Investigation on fatigue crack propagation behaviors in the thickness direction of 2519A aluminum alloy thick plate

Author:

Liu Wenhui,Hu Qiang,Chen Yuqiang,Tang Changping,Zhao Chenbing,Xiao Mingyue,Song Yufeng

Funder

Natural Science Foundation of Hunan Province

National Natural Science Foundation of China

Publisher

Elsevier BV

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials,General Materials Science,Modeling and Simulation

Reference46 articles.

1. Dynamic mechanical properties and constitutive equations of 2519A aluminum alloy;Liu;Trans Nonferrous Met Soc China,2014

2. Fisher Jr J.J., Kramer L.S., Pickens J.R. Aluminum alloy 2519 in military vehicles. Adv Mater Amp Process 2002;160:43–7. Available from: https://link.gale.com/apps/doc/A91489877/AONE?u=anon∼c869f1a7&sid=googleScholar&xid=198c2ad0.

3. Transient crack growth behavior in aluminum alloys C415–T8 and 2519–T87;Hamilton;Eng Fract Mech,1999

4. Research on fatigue life prediction and reliability of high strength and toughness aluminum alloys;Jian;J Fail Anal Prev,2020

5. An overview of fatigue in aircraft structures;Tavares;Fatigue Fract Eng Mater Struct,2017

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